Production method for a magnetostrictive torque sensor

ABSTRACT

A method produces a magnetostrictive torque sensor which detects a steering torque applied to a steering shaft by electrically detecting distortion of magnetostrictive films provided on a surface of the steering shaft. A plating step forms the magnetostrictive film on the surface of the steering shaft, and a heat treatment step heat treats the magnetostrictive film on the steering shaft. During the heat treatment step, hydrogen in the magnetostrictive film is decreased so that a hydrogen desorbing peak around 120° C. disappears when the magnetostrictive film is heated after the heat treatment step.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a Divisional of U.S. patent application Ser. No.12/007,372, filed Jan. 9, 2008, now U.S. Pat. No. 7,730,602, whichclaims priority from Japanese Patent Application No. 2007-000918 filedon Jan. 9, 2007. The disclosures of the prior applications are herebyincorporated by reference herein in their entirety.

BACKGROUND OF THE INVENTION

1. Field of the Invention

The present invention relates to a magnetostrictive torque sensor whichelectrically detects a distortion of a magnetostrictive film provided ona surface of a steering shaft, thereby detecting steering torque appliedto the steering shaft, and a production method and an evaluation methodfor the same.

2. Description of the Related Art

Magnetostrictive torque sensors are used in electric power steeringsystems for vehicles, and the electric power steering system is asupport system which, when a driver turns the steering wheel whiledriving the vehicle, has a motor cooperate therewith so as to assist thesteering effort. In the electric power steering system, themagnetostrictive torque sensor detects the steering torque caused in thesteering shaft coupled to the steering wheel by the driver turning thesteering wheel. The electric power steering system controls theauxiliary steering force that is the output from the motor based on thedetected steering torque and a vehicle speed signal from a vehicle speedsensor, which detects the speed of the vehicle, thereby reducing thesteering effort of the driver.

A magnetostrictive torque sensor has been proposed where twomagnetostrictive films of Ni—Fe alloy are provided one above the otheron the surface of the steering shaft so as to have opposite directionsof magnetic anisotropy (refer to, e.g., Japanese Patent ApplicationLaid-Open Publication No. 2004-333449). When the steering torque acts onthe steering shaft, the steering shaft is twisted, thus distorting themagnetostrictive films, and the alternating-current resistance and thelike of coils provided around the magnetostrictive films vary accordingto an inverse magnetostriction characteristic due to magneticanisotropy. The magnetostrictive torque sensor detects this change,thereby detecting the steering torque acting on the steering shaft.

As to, e.g., vehicles, forklifts, and the like, ambient temperature ofuse may be high. Due to, for example, heat from the engine such as acombustion engine or a motor, heat from a factory, and further heat fromdirect sunlight, ambient temperature of use reaches 80 to 110° C. In,particularly, vehicles used at such use ambient temperature, theauxiliary steering force may differ in magnitude between when turningthe steering wheel rightward and when turning it leftward. Inparticular, after a vehicle is left for a long time at use ambienttemperature, when turning the steering wheel while being in a stoppedstate, i.e., when performing so-called stationary steering, the drivermay realize that the auxiliary steering force differs in magnitudebetween the rightward turning and leftward turning of the steeringwheel. The cause for this is thought to be that the magnitude of thesteering torque signal detected by the magnetostrictive torque sensorshifts at use ambient temperature to be different between the rightwardturning and leftward turning of the steering wheel.

SUMMARY OF THE INVENTION

Preferably there is provided a magnetostrictive torque sensor where,even at use ambient temperature, the shift in the magnitude of thedetected steering torque signal is reduced and where the magnitude ofthe detected steering torque signal is the same for the rightwardturning and the leftward turning with the same steering effort, and aproduction method for the magnetostrictive torque sensor.

A first aspect provides a magnetostrictive torque sensor comprising: asteering shaft; and a magnetostrictive film provided on a surface of thesteering shaft of which distortion is to be electrically detected inorder to detect steering torque applied to a steering shaft, whereinafter the magnetostrictive film is removed from the surface of thesteering shaft, when a thickness of the magnetostrictive film is at 40μm, and thermal desorption gas analysis is performed thereon in whichthe magnetostrictive film is heated at a temperature rise rate of 5° C.per minute, wherein after the thermal desorption gas analysis themagnetostrictive film contains hydrogen so as to satisfy at least one ofthe following first to third conditions: the first condition that aratio of the weight of hydrogen desorbed by the heating from themagnetostrictive film by the time the magnetostrictive film reaches 150°C. to the weight of the magnetostrictive film before the heating is ator below 3 ppm; the second condition that the ratio of the weight ofhydrogen desorbed by the time the magnetostrictive film reaches 300° C.to the weight of the magnetostrictive film before the heating is at orbelow 10 ppm; and the third condition that the ratio of the weight ofhydrogen desorbed by the time the magnetostrictive film reaches 400° C.to the weight of the magnetostrictive film before the heating is at orbelow 15 ppm.

According to the first aspect, although hydrogen is mixed in themagnetostrictive film when formed, because the hydrogen content isreduced, no more hydrogen outgases from the magnetostrictive film at useambient temperature, thus reducing the shift in the magnitude of thesteering torque signal detected by the magnetostrictive torque sensor.Hence, if adjustment is made such that the magnitude of the detectedsteering torque signal is the same between when turning the steeringwheel rightward and when turning it leftward before the vehicle is used,even at use ambient temperature while the vehicle is being used, themagnitude of the detected steering torque signal can be the same withthe same steering effort between when turning the steering wheelrightward and when turning it leftward. Thus, a driver can steer thevehicle comfortably without feeling unease.

A second aspect provides a production method for a magnetostrictivetorque sensor which detects steering torque applied to a steering shaftby electrically detecting distortion of a magnetostrictive film providedon a surface of the steering shaft, comprising: a plating step offorming the magnetostrictive film on the surface of the steering shaft;and a heat treatment step of heat-treating the magnetostrictive film;removing the magnetostrictive film after the heat treatment step fromthe surface of the steering shaft; performing a thermal desorption gasanalysis thereon is performed in which the magnetostrictive film isheated at a temperature rise rate of 5° C. per minute, when a thicknessof the magnetostrictive film is 40 μm, wherein hydrogen in themagnetostrictive film is reduced in amount by the heat treatment step soas to satisfy at least one of the following conditions: a condition thata ratio of the weight of hydrogen desorbed by the heating from themagnetostrictive film by the time the magnetostrictive film reaches 150°C. to the weight of the magnetostrictive film before the heating is ator below 3 ppm; a condition that the ratio of the weight of hydrogendesorbed by the time the magnetostrictive film reaches 300° C. to theweight of the magnetostrictive film before the heating is at or below 10ppm; and a condition that the ratio of the weight of hydrogen desorbedby the time the magnetostrictive film reaches 400° C. to the weight ofthe magnetostrictive film before the heating is at or below 15 ppm.

According to the second aspect, although hydrogen is mixed into themagnetostrictive film in the plating step, because the heat treatmentstep can reduce the content of hydrogen, no more hydrogen is desorbedfrom the magnetostrictive film at use ambient temperature, and hence themagnitude of the steering torque signal detected by the magnetostrictivetorque sensor does not shift.

A third aspect provides a production method based on the second aspect,further comprising: a condition setting step of setting a heat treatmenttemperature of the magnetostrictive film in the heat treatment step andheat treatment time for which to maintain the heat treatmenttemperature, wherein in the condition setting step, the heat treatmenttime required to reduce the amount of hydrogen in the magnetostrictivefilm so as to satisfy the at least one condition can be set according tothe heat treatment temperature, or the heat treatment temperaturerequired to reduce the amount of hydrogen in the magnetostrictive filmso as to satisfy the at least one condition can be set according to theheat treatment time.

Therefore, the heat treatment temperature and the heat treatment time ofthe heat treatment step can be set according to the type ofheat-treating apparatus. For example, if a low-temperature thermostaticbath of which the heat treatment temperature cannot be set at a hightemperature is used as the heat-treating apparatus, the heat treatmenttime may be set according to the low heat treatment temperature of thethermostatic bath. If a hardening or annealing apparatus of which theheat treatment temperature is set at a high temperature is used as theheat-treating apparatus, the heat treatment time may be set according tothe high heat treatment temperature. As such, degrees of freedom inselecting as the heat-treating apparatus can be increased in number.

The heat treatment step preferably comprises a plurality of heattreatments different in the heat treatment temperature or heattreatments the times of which the heat treatment time is divided into.With such a multiple stage heat treatment, the amount of hydrogen can bereduced at each stage. Hence, the heat treatment whose primary objectiveis not to reduce the amount of hydrogen can also be used as a stage of aheat treatment for reducing the amount of hydrogen.

In the heat treatment step, in order to give magnetic anisotropy to themagnetostrictive film, while torque is being applied to the steeringshaft, preferably the magnetostrictive film provided on the surface ofthe steering shaft is heated. The amount of hydrogen can be reduced withgiving magnetic anisotropy to the magnetostrictive film.

In the heat treatment step, the magnetostrictive film is preferably heattreated by high frequency heating. Since the high frequency heating canheat the outer layer of an object, only the magnetostrictive film can beheated without heating the steering shaft because the magnetostrictivefilm is provided on the surface of the steering shaft.

A fourth aspect of the present invention provides evaluation method fora magnetostrictive torque sensor which detects steering torque appliedto a steering shaft by electrically detecting distortion of amagnetostrictive film provided on a surface of the steering shaft,comprising: removing the magnetostrictive film from the surface of thesteering shaft; performing a thermal desorption gas analysis thereon inwhich the magnetostrictive film is heated at a temperature rise rate of5° C. per minute; evaluating variation over time in a magneticcharacteristic of the magnetostrictive film when a thickness of themagnetostrictive film is 40 μm, by determining whether at least one ofthe following conditions has been satisfied: a condition that a ratio ofthe weight of hydrogen desorbed by the heating from the magnetostrictivefilm by the time the magnetostrictive film reaches 150° C. to the weightof the magnetostrictive film before the heating is at or below 3 ppm; acondition that the ratio of the weight of hydrogen desorbed by the timethe magnetostrictive film reaches 300° C. to the weight of themagnetostrictive film before the heating is at or below 10 ppm; and acondition that the ratio of the weight of hydrogen desorbed by the timethe magnetostrictive film reaches 400° C. to the weight of themagnetostrictive film before the heating is at or below 15 ppm.

According to the fourth aspect, because variation over time in amagnetic characteristic of the magnetostrictive film depends on theweight of hydrogen that can be desorbed, in the thermal desorption gasanalysis, by measuring the weight of hydrogen desorbed, the magneticcharacteristic of the magnetostrictive film can be predicted. Based onthis prediction, variation over time in the magnetic characteristic ofthe magnetostrictive film can be evaluated through the abovedetermination. Therefore, the magnetostrictive film with smallervariation over years in the magnetic characteristic can be provided.

BRIEF DESCRIPTION OF THE DRAWINGS

For a more complete understanding of the present invention and theadvantages thereof, reference is now made to the following descriptiontaken in conjunction with the accompanying drawings wherein:

FIG. 1 is an illustration showing an electric power steering systemhaving a magnetostrictive torque sensor according to an embodiment ofthe present invention;

FIG. 2 is a diagram showing the configuration of the magnetostrictivetorque sensor and accompanied units in the electric power steeringsystem according to the present embodiment;

FIG. 3 is a block diagram of a motor current control unit and abrushless motor according to the present embodiment;

FIG. 4 shows the output characteristics of a first main coil and a firstsub coil placed on a first magnetostrictive film and of a second maincoil and a second sub coil placed on a second magnetostrictive film;

FIG. 5 shows the output characteristics of the first main coil, firstsub coil, second main coil and second sub coil, and the outputcharacteristics of a VT3 main signal, a VT3 sub signal, detected torquesignal, and failure detection signal that are plotted only over the userange Rt of FIG. 4;

FIG. 6A shows the output characteristics of the magnetostrictive torquesensor before being left at use ambient temperature;

FIG. 6B shows the output characteristics of the magnetostrictive torquesensor after being left at use ambient temperature;

FIG. 7 shows a temperature profile of the amount of hydrogen desorbedfrom the first magnetostrictive film before heat treatment measuredaccording to thermal desorption gas analysis;

FIG. 8 shows a temperature profile of the desorption rate of hydrogendesorbed from the first magnetostrictive film before heat treatmentmeasured according to thermal desorption gas analysis;

FIG. 9A shows the distribution of hydrogen atoms related to thedesorption of hydrogen of mode 1 in FIG. 8 in a unit lattice of thefirst magnetostrictive film;

FIG. 9B shows the distribution of hydrogen atoms related to thedesorption of hydrogen of mode 2 in a unit lattice of the firstmagnetostrictive film;

FIG. 10 is a front view of a heat-treating apparatus according to thepresent embodiment;

FIG. 11A is a side view of a steering shaft;

FIG. 11B is a side view of the steering shaft placed in theheat-treating apparatus;

FIG. 12 shows a temperature profile of the amount of hydrogen desorbedfrom the first magnetostrictive film after heat treatment measuredaccording to thermal desorption gas analysis;

FIG. 13 is a chart of the change rates of the gradient (sensitivity) andmiddle point of the detected torque signal before and after being leftat use ambient temperature against the desorbed hydrogen amount for 400°C. when heated to 400° C. in thermal desorption gas analysis;

FIG. 14 shows an allowable area through which a temperature profile thatthe first magnetostrictive film should satisfy in thermal desorption gasanalysis passes; and

FIG. 15 is a chart showing a relationship between heat treatmenttemperature and heat treatment time when the desorbed hydrogen amount isthe same.

DETAILED DESCRIPTION OF THE INVENTION

An embodiment of the present invention will be described in detail belowwith reference to the drawings as needed. In the figures, the samereference numerals indicate common parts with duplicate descriptionthereof being omitted.

FIG. 1 is a diagram of the entire configuration of an electric powersteering system (EPS) 1 according to an embodiment of the presentinvention. A steering wheel 2 is coupled to the upper end of a steeringshaft 21 via universal joints 13 a, 13 b. A pinion gear 11 b is securedto the lower end of the steering shaft 21. The pinion gear 11 b engagesa rack gear 11 a, and the rack gear 11 a and the pinion gear 11 b form arack-pinion gear 11. The rack-pinion gear 11 converts steering torque Tsof the steering shaft 21 into thrust of an axis direction of a rackshaft 6. The rack gear 11 a is made by cutting into the rack shaft 6.

A ball screw 7 is also made by cutting into the rack shaft 6, and a ballnut is provided on the inner side of a worm wheel gear 5 b. The ballscrew 7 engages the ball nut via a plurality of balls. The outer teethof the worm wheel gear 5 b engage a worm gear 5 a. The worm gear 5 a iscoupled to the rotation shaft of a brushless motor 4. The brushlessmotor 4 assists the driver to steer with power. The worm gear 5 a andthe worm wheel gear 5 b form a decelerating device 5. The deceleratingdevice 5 doubles auxiliary torque AH that the brushless motor 4generates. The ball screw 7 converts the doubled auxiliary torque AHinto thrust in the axis direction of the rack shaft 6. One ends of tierods 14 are fixed to opposite ends of the rack shaft 6, and a tire 10 asa front wheel is attached to the other end of each tie rod 14.

The rack shaft 6 is supported at its one end by a bearing 27 via theball screw 7 and at the other end by a rack guide (not shown) and isheld in a steering gear box 12 so as to be able to freely move in theaxis direction without rotating. The steering shaft 21 is rotatably heldin the steering gear box 12 by bearings 24, 25, 26.

A tightener 22 is provided on the steering shaft 21 to couple theuniversal joint 13 b and the steering shaft 21. Further, on the steeringshaft 21, a seal 23 is provided to seal the steering shaft 21 to thesteering gear box 12, and also a flat surface 29 and a fixing portion 28are provided.

A magnetostrictive torque sensor 3 is provided on the steering shaft 21.The magnetostrictive torque sensor 3 detects steering torque Ts input bya driver through the steering wheel 2. The magnetostrictive torquesensor 3 has annular first and second magnetostrictive films 3 a, 3 bformed around the steering shaft 21. An Fe—Ni-based or Fe—Cr-basedmagnetostrictive material is suitable for the first and secondmagnetostrictive films 3 a, 3 b. The first and second magnetostrictivefilms 3 a, 3 b are formed by plating, vapor deposition, or the like onthe steering shaft 21 or the like, for example, on the surface of thesteering shaft 21 or a hollow pipe into which the steering shaft 21 isforce fitted. The first and second magnetostrictive films 3 a, 3 b maybe integrated with the steering shaft 21, or may be formed beforehandand bonded to the steering shaft 21 by an adhesive.

Further, the magnetostrictive torque sensor 3 has a first main coil 31and a first sub-coil 32 around the first magnetostrictive film 3 a andalso a second main coil 33 and a second sub-coil 34 around the secondmagnetostrictive film 3 b.

The steering torque Ts is generated by the driver turning the steeringwheel 2 and transmitted to the steering shaft 21. The transmittedsteering torque Ts is detected by the magnetostrictive torque sensor 3,and a VT1 main signal (VT1 main) as a detection signal is output fromthe first main coil 31. Also, a VT1 sub signal (VT1 sub) is output fromthe first sub-coil 32; a VT2 main signal (VT2 main) is output from thesecond main coil 33; and a VT2 sub signal (VT2 sub) is output from thesecond sub-coil 34. The VT1 main signal, VT1 sub signal, VT2 mainsignal, and VT2 sub signal are input to a controller ECU. The controllerECU comprises a computer and receives a vehicle speed signal V and thelike from a vehicle speed sensor 8 detecting the speed of the vehicle.Also, the controller ECU receives a measured current signal Do obtainedby measuring the motor electric current flowing through the brushlessmotor 4, a motor rotation angle signal “a” obtained by measuring therotation angle of the rotor of the brushless motor 4, and the like.

The controller ECU outputs a motor current signal D to make thebrushless motor 4 operate based on the received VT1 main signal, VT1 subsignal, VT2 main signal, VT2 sub signal, vehicle speed signal V,measured current signal Do, motor rotation angle signal “a”, and thelike.

The brushless motor 4 outputs the auxiliary torque AH to assist thesteering torque Ts according to the motor current signal D, and theauxiliary torque AH is transmitted to the rack shaft 6 via thedecelerating device 5, by which it is converted to linear motion. Also,the steering torque Ts generated directly by the driver is transmittedto the rack shaft 6 via the rack-pinion gear 11, by which it isconverted to linear motion.

The linear motion from the steering torque Ts transmitted to the rackshaft 6 and the linear motion from the auxiliary torque AH are combinedto move the tie rods 14, thereby changing the travel direction of thetires 10. By combining the auxiliary torque AH with the steering torqueTs, the steering torque Ts necessary for the driver to steer can bereduced. The turning angle θ of the steering wheel 2 rotates the traveldirection of the tires 10 through α.

For example, for easiness to understand, it is assumed that Ts is thevalue of the steering torque Ts, AH is the value of the auxiliary torqueAH, and a constant kA is a coefficient of the auxiliary torque AH. ThenAH=kA×Ts. It is assumed that Tp is pinion torque, which is a load. Thenthe pinion torque Tp is a sum of steering torque Ts and auxiliary torqueAH (Tp=Ts+AH), and hence Ts=Tp/(1+kA). Therefore, the steering torque Tsis 1/(1+kA) times the pinion torque Tp, where kA≦0, and smaller than thepinion torque Tp, thus reducing the steering torque Ts. Although in theabove the kA is assumed to be a constant for easiness to understand, thekA preferably decreases as the vehicle speed increases. By this means,even if a load to rotate the tires 10 through α relative to the roadsurface decreases as the vehicle's traveling speed becomes higher, thesteering torque Ts required to rotate the tires 10 through α can belarge enough to give a feeling of reaction.

FIG. 2 is a block diagram of the magnetostrictive torque sensor 3 andits neighbors in the electric power steering system 1. As shown in FIG.2, the controller ECU has an interface 15. The interface 15 has aconverter 35 and an amplifier circuit AMP. The amplifier AMP has anamplifier 35 a for amplifying the VT1 main signal, an amplifier 35 b foramplifying the VT2 main signal, an amplifier 35 c for amplifying the VT1sub signal, and an amplifier 35 d for amplifying the VT2 sub signal. Theconverter 35 has a VT3 main calculator (operational amplifier) 36 forcalculating a VT3 main signal (VT3 main) and a VT3 sub calculator(operational amplifier) 37 for calculating a VT3 sub signal (VT3 sub).Further, the controller ECU has a detected torque signal calculator(operational amplifier) 16 for calculating a detected torque signal VSfrom the VT3 main signal and VT3 sub signal and an adder 17 for addingthe VT3 sub signal to the VT3 main signal to obtain a failure detectionsignal VE. Further, the controller ECU has a motor current control unit18 for outputting a motor current D to make the brushless motor 4operate based on the detected torque signal VS, vehicle speed signal V,measured current signal Do, and motor rotation angle signal “a”, and afailure detector 19 for detecting a failure in the magnetostrictivetorque sensor 3.

FIG. 3 is a block diagram of the motor current control unit 18 and thebrushless motor 4. As shown in FIG. 3, the motor current control unit 18has an assist controller 51, a filter F, a response improving(differential) controller 52, a steering shaft rotation speed calculator54, a damper controller 53, a three-phase conversion adder-subtractor55, and a PID controller 56.

The assist controller 51 determines a motor current signal DT to outputthe auxiliary torque AH based on the detected torque signal VS andvehicle speed signal V. The motor current signal DT needs to be madelarger as the detected torque signal VS becomes larger, and converselybe made smaller as the vehicle speed signal V becomes larger. Further,an area where the motor current signal DT is constant exists in the areawhere the detected torque signal VS is large. Thus, when the vehiclespeed signal V becomes larger, a definite feeling of reaction to thesteering torque can be given. This corresponds to decreasing the kA asthe vehicle speed increases as mentioned above. In order to determinethe motor current signal DT, the motor current signal DT is preferablydefined as a function f(VS, V) with the detected torque signal VS andvehicle speed signal V as arguments, and the function may be defined asa table not being limited to an equation.

The filter F can improve the response and stability of the brushlessmotor 4 and specifically calculates a differential value F of thedetected torque signal VS. The response improving (differential)controller 52 adjusts a gain kT for the calculated differential value Faccording to the vehicle speed signal V. The gain kT tends to bedecreased as the vehicle speed signal V becomes larger. In order toadjust the gain kT, the gain kT is preferably defined as a function f(V)with the vehicle speed signal V defined as an argument, and the functionmay be defined as a table not being limited to an equation. A motorcurrent signal DTD can be obtained by multiplying the detected torquesignal VS, the differential value F, and the gain kT (DTD=VS×F×kT).

The steering shaft rotation speed calculator 54 calculates a motorrotation (steering) speed signal S by differentiating the motor rotationangle signal a. The damper controller 53 determines a motor currentsignal Ds to be subtracted from the motor current signal based on themotor rotation speed signal S and the vehicle speed signal V. The motorcurrent signal Ds tends to be made larger as either of the motorrotation speed signal S and the vehicle speed signal V becomes larger.The three phase converting adder-subtractor 55 subtracts the largermotor current signal Ds as the vehicle speed signal V becomes larger andsubtracts the larger motor current signal Ds as the rotation speed ofthe brushless motor 4, i.e., the motor rotation speed signal S becomeslarger, thus producing a damper effect. This improves convergencecharacteristic of the settling of the steering wheel 2 and thus improvesthe stability of the vehicle when traveling at high speed. In order todetermine the motor current signal Ds, the motor current signal Ds ispreferably defined as a function f(S, V) with the motor rotation speedsignal S and vehicle speed signal V defined as arguments, and thefunction may be defined as a table not being limited to an equation.

The three phase converting adder-subtractor 55 adds the motor currentsignal DT and the motor current signal DTD and subtracts the motorcurrent signal Ds, thereby calculating a target torque current signal.The brushless motor 4 comprises a brushless motor body 40, a resolver 41and current sensors 42, 43. The resolver 41 detects the motor rotationangle of the rotor of the brushless motor body 40 and transmits themotor rotation angle signal a. The current sensors 42, 43 transmit themeasured current signal Do obtained by measuring the motor currentflowing through the brushless motor body 40. In the three phaseconverting adder-subtractor 55, the measured current signal Do havingthree phases is dq-converted by the motor rotation angle signal “a”.

The PID controller 56 outputs a motor current D to the brushless motorbody 40 so as to make the dq-converted measured current signal Docoincide with the target torque current signal calculated by the threephase converting adder-subtractor 55.

FIG. 4 shows the output characteristics of the VT1 main signal, VT1 subsignal, VT2 main signal, and VT2 sub signal.

While alternating currents are flowing through the first and secondmagnetostrictive films 3 a, 3 b, when torque is applied, variations inpermeability that is the magnetostrictive characteristic of the firstand second magnetostrictive films 3 a, 3 b are detected by means of thefirst main coil 31, the first sub-coil 32, the second main coil 33, andthe second sub-coil 34 in the form of the output characteristics f(theVT1 main signal, VT1 sub signal, VT2 main signal, and VT2 sub signal).

The output characteristic VTO produced with the first and secondmagnetostrictive films 3 a, 3 b before magnetic anisotropy is given isan output characteristic (e.g., an impedance characteristic) almostsymmetric with respect to the acting directions of the torque (rightwardturn (+), leftward turn (−)). Then, rightward turn torque +To andleftward turn torque −To that are sufficiently larger than a use rangeRt are made to remain in the first and second magnetostrictive films 3a, 3 b, thereby giving magnetic anisotropy thereto. The outputcharacteristics of the first magnetostrictive film 3 a given magneticanisotropy by the torque +To are the VT1 main signal and VT1 sub signal,and the output characteristics of the second magnetostrictive film 3 bgiven magnetic anisotropy by the torque −To are the VT2 main signal andVT2 sub signal.

For the use range Rt, an operation expressed as “VT3 main signal=VT1main signal−VT2 main signal” and an operation expressed as “−VT3 subsignal=VT1 sub signal−VT2 sub signal” are performed in the VT3 maincalculator 36 and the VT3 sub calculator 37 (see FIG. 2). Theseoperations enable detecting the acting direction and magnitude of thetorque and improve sensitivity (the gradient of the graph in FIG. 4). Inorder to detect a failure in the magnetostrictive torque sensor 3, thefailure detection signal VE is defined as (VT1 main signal+VT2 mainsignal)/2 or (VT1 sub signal+VT2 sub signal)/2. If normal, they arealmost constant. A use range Rvt of an appropriate allowable width withan output maximum VTmax and an output minimum VTmin as upper and lowerlimits can be set. If the failure detection signal VE is not in betweenthe output maximum VTmax, the upper limit, and the output minimum VTmin,the lower limit, it can be determined that a failure has occurred. Thefailure detection signal VE is often set at about 2.5 V in terms ofvoltage.

FIG. 5 shows the output characteristics of the VT1 main signal, VT1 subsignal, VT2 main signal, VT2 sub signal, VT3 main signal, VT3 subsignal, the detected torque signal VS, and the failure detection signalVE that are plotted only over the use range Rt. The VT3 main signal iscalculated in the VT3 main calculator 36 by subtracting the VT2 mainsignal from the VT1 main signal and multiplying the subtracted value bya coefficient k (VT3 main signal=k×(VT1 main signal−VT2 main signal)).Further, the VT3 main signal is shifted by the VT3 main calculator 36 soas to be at 2.5 V when the torque is at zero.

The VT3 sub signal is calculated in the VT3 sub calculator 37 bysubtracting the VT1 sub signal from the VT2 sub signal and multiplyingthe subtracted value by a coefficient k (VT3 sub signal=k×(VT2 subsignal−VT1 sub signal)). Further, the VT3 sub signal is shifted by theVT3 sub calculator 37 so as to be at 2.5 V when the torque is at zero.

The detected torque signal VS is calculated in the detected torquesignal calculator 16 by subtracting the VT3 sub signal from the VT3 mainsignal (VS=VT3 main signal−VT3 sub signal). Even if use ambienttemperature or the magnetic environment varies and thus the VT1 mainsignal, VT2 main signal, VT1 sub signal, and VT2 sub signal vary, theirvariations can be cancelled out because they vary in the same way. Whenthe torque is at zero, both the VT3 main signal and the VT3 sub signalare at 2.5 V. Hence, the detected torque signal VS can also be at zerowhen the torque is at zero. From the detected torque signal VS, theacting directions of the torque (rightward turn (+), leftward turn (−))and its magnitude can be detected. Because the detected torque signal VSis large in the gradient of its graph of FIG. 5, the magnitude of thetorque can be detected with high sensitivity.

The failure detection signal VE is calculated in the adder 17 by addingthe VT3 sub signal to the VT3 main signal and multiplying the addedvalue by ½ (VE=(VT3 main signal+VT3 sub signal)/2). The failure detector19 determines whether the failure detection signal VE is within the userange Rvt, and if true, determines being normal and if not, determinesthat a failure has occurred. To be specific, the failure detector 19determines whether the failure detection signal VE is greater than theoutput maximum VTmax and if greater, outputs the result indicating theoccurrence of a failure and if not, outputs the result indicating beingnormal. Likewise, the failure detector 19 determines whether the failuredetection signal VE is greater than the output minimum VTmin and ifgreater, outputs the result indicating being normal and if not, outputsthe result indicating the occurrence of a failure.

In the above, the structure of the magnetostrictive torque sensor 3 andthe mechanism of detecting torque have been described. In the below, onthe basis of the above description there will be described thephenomenon that when performing so-called stationary steering, theauxiliary steering force differs in magnitude between the rightwardturning and leftward turning of the steering wheel, which poses aproblem.

As shown in FIG. 6A, when the magnetostrictive torque sensor 3 is placedin the atmosphere of, e.g., 20° C. in temperature, which is not subjectto the use ambient temperature, because initially steering torque is notapplied, the torque is at zero and the VT3 main signal and the VT3 subsignal intersect at the middle point Vd of the use range Rvt. Hence, thedetected torque signal VS passes through the origin. Here, it is assumedthat an output value Va is obtained when torque +T1 is applied. Then, iftorque −T1 of the same magnitude in the direction opposite to that ofthe torque +T1 is applied, an output value −Va of the same magnitude inthe direction opposite to that of the output value Va can be obtained.Further, the value of the failure detection signal VE is equal to themiddle point Vd and hence within the use range Rvt.

Here, it is assumed that as shown in FIG. 6B, after the magnetostrictivetorque sensor 3 is subjected to the use ambient temperature or left inthe atmosphere of, e.g., 110° C. in temperature for about 400 hours, forexample, the VT3 main signal has drifted to a greater degree than theVT3 sub signal. Then, the output value Ve at the intersection of the VT3main signal and the VT3 sub signal becomes higher by Vf than the middlepoint Vd and higher than VTmax. Also, the value of the failure detectionsignal VE becomes the same as the output value Ve and hence is notwithin the use range Rvt. Thus, a failure is detected. When the torqueis at zero, the detected torque signal VS does not pass through theorigin, and thus an output value Vg is output. Although the torque −T1of the same magnitude in the direction opposite to that of the torque+T1 is applied because application of the torque +T1 provides an outputvalue Vb, an output value of the same magnitude in the directionopposite to that of the output value Vb is not obtained, but an outputvalue Vc of different magnitude is obtained. This difference causes thephenomenon that the auxiliary steering force differs in magnitudebetween the rightward turning and leftward turning of the steeringwheel.

The detected torque signal VS is output at the output value Vg even whenthe torque is at zero. Hence, when steering torque is not applied, thatis, when not turning the steering wheel, the detected torque signal VSis at the output value Vg, and hence the motor current D set by themotor current control unit 18 is expected to flow through the brushlessmotor 4.

Since the drifts of the VT3 main signal and of the VT3 sub signal arecaused by the drift of the VT1 main signal, VT1 sub signal, VT2 mainsignal, and VT2 sub signal, the drifts are thought to be caused by somechange in the quality of the first and second magnetostrictive films 3a, 3 b at the use ambient temperature.

Accordingly, as to the first and second magnetostrictive films 3 a, 3 b,the hydrogen amount in samples was measured according to thermaldesorption gas analysis (TDS). First, the first and secondmagnetostrictive films 3 a, 3 b of, e.g., Ni—35% Fe in composition andof 40 μm in thickness were formed on the steering shaft 21 by, e.g.,electroplating, and thereafter the first and second magnetostrictivefilms 3 a, 3 b were removed mechanically from the steering shaft 21. Theremoved first and second magnetostrictive films 3 a, 3 b were cut intoparts of about 30 mm² in surface area to make samples. The thicknessesof the removed first and second magnetostrictive films 3 a, 3 b were thesame 40 μm as that after the formation. Next, the samples were put in aglass-made ampoule, which was evacuated and heated to 500° C. at a riserate of 5° C. per minute. Pressure variation in the ampoule being heatedwas measured with a Pirani gage, and the number of moles of hydrogendesorbed from the samples was obtained. Further, the ratio x of theweight of desorbed hydrogen gas to the weight of the samples (a desorbedhydrogen amount) was calculated. The results of the calculation areshown in FIG. 7. The horizontal axis represents the sample temperature twhen heating the samples at the rise rate of 5° C. per minute, and thevertical axis represents the desorbed hydrogen amount x. It was foundthat the desorbing rate of hydrogen rises rapidly around 100° C. anddesorbing continues until around 400° C. Further, it was confirmed witha mass spectrometer that all of desorbed gas due to heating up to 500°C. was hydrogen (H₂).

Next, as shown in FIG. 8, by differentiating the desorbed hydrogenamount x with respect to the sample temperature t, the desorbing rate(dx/dt) was calculated. It is thought that the profile of the desorbingrate has the distribution for hydrogen of mode 1 having its peak around120° C. and that for hydrogen of mode 2 having peaks over a wide rangeof 250 to 350° C. overlapping. There is a sharp peak around 400° C.,which is thought to indicate hydrogen desorbed due to phase change orthermal decomposition because the peak did change through heat treatmentat temperatures below the peak's temperature. The hydrogen of mode 1 isthought to be the main cause for the change in state of themagnetostrictive films because the desorbed hydrogen amount decreasesand the peak's temperature shifts toward the high temperature side astime elapses from the plating. In order to accelerate the desorbing ofthe hydrogen of mode 1 to stabilize the magnetostrictive films, themagnetostrictive films need to be heat treated at as high temperature aspossible without damaging the characteristics of the magnetostrictivefilms and their base material, which temperature is preferably set atannealing temperature for material for structure. If heat treated at lowtemperature, heat treatment time needs to be extended. For use in a hightemperature environment such as the engine, the hydrogen of mode 2 thatis desorbed at even higher temperature is also preferably stabilized,and the magnetostrictive films may be heat treated at 250° C. or above.

Thus, if the heat treatment step comprises a plurality of heattreatments different in the heat treatment temperature or heattreatments of which the heat treatment time is divided into, the heattreatments may have peak temperatures of substantially 120° C. and 400°C., respectively.

FIG. 9A shows a state where the hydrogen of mode 1 is contained in thefirst or second magnetostrictive film 3 a, 3 b. Hydrogen atoms H existby solution between lattice points (or in spaces) of metal atoms Mforming the first or second magnetostrictive film 3 a, 3 b. Theactivation energy for this hydrogen atom to move is so small as to moveaway at about room temperature. Therefore, hydrogen outgases indiffusion from the first and second magnetostrictive films 3 a, 3 b evenin the market environment.

FIG. 9B shows a state where the hydrogen of mode 2 is contained in thefirst or second magnetostrictive film 3 a, 3 b. A large amount ofhydrogen that is generated in forming the films causes the generation ofvacancies, and forms vacancy-hydrogen clusters to be in a metastablestate, which is higher in binding energy than in the case of existing bysolution between the lattice points, and hence hydrogen movement(diffusion) occurs at higher temperature. It was found that hydrogenoutgassing from the vacancy-hydrogen clusters rapidly increases in atemperature range of 200° C. or above.

Due to the diffusive movement of hydrogen atoms H of modes 1 and 2,changes in internal stress occur in the first and secondmagnetostrictive films 3 a, 3 b, thus changing their magnetostrictivecharacteristic. Further, as to the mode 2, it is thought that an excessof vacancies 57 exist, hence facilitating the diffusive movement ofmetal atoms M such as nickel (Ni) atoms and iron (Fe) atoms and thatalso by this diffusive movement, internal stress changes thus changingthe magnetostrictive characteristic.

Hence, in order not to let the magnetostrictive characteristic change,it is thought that hydrogen atoms H and vacancies 57 need to beprevented from diffusively moving. Accordingly, in order to preventhydrogen atoms H and vacancies 57 from diffusively moving at use ambienttemperature, hydrogen atoms H and vacancies 57 in the first and secondmagnetostrictive films 3 a, 3 b need to be reduced in number, andparticularly hydrogen atoms H need to be desorbed from the first andsecond magnetostrictive films 3 a, 3 b. Accordingly, in the vehicleproduction process, the first and second magnetostrictive films 3 a, 3 bare heat-treated in order that hydrogen is desorbed from the first andsecond magnetostrictive films 3 a, 3 b, which reduces the concentrationof hydrogen in the first and second magnetostrictive films 3 a, 3 b.

In the below, the heat treatment process for the first and secondmagnetostrictive films 3 a, 3 b will be described.

FIG. 10 shows a heat-treating apparatus 61 used in the heat treatmentprocess. A plurality of the steering shafts 21 having the first andsecond magnetostrictive films 3 a, 3 b formed thereon are put in theheat-treating apparatus 61 and can be heated under the same conditionsat the same time. The steering shafts 21 are put in a chamber 62 and areinserted into a mount 63 placed in the chamber 62 so as to standupright. Then, the first and second magnetostrictive films 3 a, 3 b areheated using a power supply 64. One of the steering shafts 21 is used asa TDS sample 65 for TDS measurement to evaluate how much hydrogen thatcan be desorbed is contained in the first and second magnetostrictivefilms 3 a, 3 b. The other steering shafts 21 are evaluated in terms ofhow much the magnetostrictive characteristic changes at use ambienttemperature.

The first and second magnetostrictive films 3 a, 3 b need to be givenmagnetic anisotropy. As the method of giving magnetic anisotropy thereis a method in which the creep characteristic of the first and secondmagnetostrictive films 3 a, 3 b themselves is used. Torques of the samemagnitude in opposite rotational directions are applied respectively tothe first and second magnetostrictive films 3 a, 3 b at the same time,the first and second magnetostrictive films 3 a, 3 b are heated to about300 to 400° C. Then, after the first and second magnetostrictive films 3a, 3 b are left at room temperature to be cooled, the application of thetorques is stopped.

When bonded to the steering shaft 21, the first and secondmagnetostrictive films 3 a, 3 b are bonded onto the steering shaft 21 towhich torques of the same magnitude in opposite rotational directionsare being applied simultaneously, and then the only stopping applicationof the torques can complete the process. As such, in methods of givingmagnetic anisotropy, the first and second magnetostrictive films 3 a, 3b need not necessarily be heated.

However, the method of giving magnetic anisotropy, where heated,functions also as the heat treatment process, and hence with givingmagnetic anisotropy, hydrogen can be desorbed to reduce the amount ofresidual hydrogen.

A method of giving magnetic anisotropy will be described in detail belowusing FIGS. 11A and 11B.

First, as shown in FIG. 11B, high frequency coils 67 a and 67 b throughwhich alternating currents of high frequency flow are wound respectivelyaround the first and second magnetostrictive films 3 a, 3 b on thesteering shaft 21. The tightener 22 shown in FIG. 11A is attached andfixed to a fastener 65 a, and the fixing portion 28 is attached andfixed to a fastener 65 b. A torque applying jig 66 is made to engage aflat surface 29 provided between the first and second magnetostrictivefilms 3 a, 3 b to be fixed to the steering shaft 21 so as to twist thesteering shaft 21, thereby applying torque thereto. The magnitude of theapplied torque corresponds to that of torque +To of FIG. 4 and ispreferably 1.5 or greater times the upper limit of the use range Rt. Tobe specific, torque of about 15 to 100 Nm in magnitude is applied. Bythis torque acting on the steering shaft 21, torques in oppositedirections act on the first and second magnetostrictive films 3 a, 3 b.While applying torque, alternating currents of high frequency are madeto flow through the high frequency coils 67 a and 67 b simultaneouslyfor about 1 to 10 sec. By this energizing, the first and secondmagnetostrictive films 3 a, 3 b are heated to creep, and thus thetorques in opposite directions are released. The advantage of this highfrequency heating (HFH) is that while the first and secondmagnetostrictive films 3 a, 3 b are heated, the steering shaft 21 ishardly heated. Hence, while in the heat treatment the temperature of thefirst and second magnetostrictive films 3 a, 3 b rises to, e.g., 400° C.by the high frequency heating, the steering shaft 21 is not heated andhence is not subject to the creep or transition in crystal structure.Further, it is thought that this high frequency heating can alsofunction as the heat treatment process for reducing the concentration ofhydrogen in the first and second magnetostrictive films 3 a, 3 b.

Finally, with the torque being applied, the temperature of the first andsecond magnetostrictive films 3 a, 3 b is lowered to room temperature.The torque applying jig 66 is detached from the flat surface 29 to stopapplying the torque from the torque applying jig 66 acting on thesteering shaft 21. By this, torques in opposite directions from thesteering shaft 21 act on the first and second magnetostrictive films 3a, 3 b, thereby giving so-called magnetic anisotropy thereto.

In this way, the heat treatment process was performed by the highfrequency heating (HFH), and the TDS sample 65 and output change ratemeasurement samples 66 were obtained. The heat treatment conditions inhigh frequency heating were the heat treatment temperature of 400° C.and the heat treatment time of 1 sec to 10 sec for the first and secondmagnetostrictive films 3 a, 3 b.

The measurement according to the thermal desorption gas analysis wasperformed on the TDS sample 65, which resulted in the graphs of FIG. 12.The measurement was conducted using the same procedure as describedreferring to FIG. 7. In FIG. 12, the spectrum labeled “400° C. (HFH)” isa spectrum of the first and second magnetostrictive films 3 a, 3 b afterthe heat treatment process by the high frequency heating (HFH). Thespectrum labeled “before heat treatment” is a spectrum of the first andsecond magnetostrictive films 3 a, 3 b before the heat treatment processand corresponds to the spectrum of FIG. 7.

In FIG. 12, the spectrum labeled “400° C. (HFH)+2 hr annealing at 180°C.” indicates the case where two stages of heat treatment processes wereperformed. The first stage is a heat treatment process by the highfrequency heating (HFH) for also giving magnetic anisotropy, and thesubsequent second stage of a heat treatment process is annealing of 180°C. in heat treatment temperature and two hours in heat treatment timeusing the heat-treating apparatus 61.

The measurement according to the thermal desorption gas analysis showsthat the heat treatment process by the high frequency heating reducedthe desorbed hydrogen amount, when heated from room temperature to 500°C., by 12 ppm as compared with the case of not performing heattreatment. Adding the annealing further reduced the desorbed hydrogenamount, resulting in the 14 ppm reduction as compared with the case ofnot performing heat treatment.

As seen from this, even if the heat treatment process is in the form ofa plurality of heat treatments that differ in heat treatment temperatureor heat treatments of which heat treatment time is divided into such asthe magnetic anisotropy giving process and the annealing process, ineach stage of a heat treatment, the amount of hydrogen can be reduced.Hence, the heat treatment whose primary objective is not to reduce theamount of hydrogen can also be used as a stage of a heat treatment forreducing the amount of hydrogen.

Moreover, since performing the heat treatment process can reduce thedesorbed hydrogen amount as compared with the case of not performingheat treatment, hydrogen is desorbed from the first and secondmagnetostrictive films 3 a, 3 b in the heat treatment process. Thus, theamount of hydrogen contained in the first and second magnetostrictivefilms 3 a, 3 b is reduced. Hence, in the measurement according to thethermal desorption gas analysis, the amount x of desorbed hydrogen isreduced. Therefore, it is thought that although the heat-treated firstand second magnetostrictive films 3 a, 3 b are placed at use ambienttemperature, the amount x of desorbed hydrogen is reduced as in themeasurement according to the thermal desorption gas analysis. Since theamount x of desorbed hydrogen at use ambient temperature is reduced, theoccurrence of the diffusive movement of hydrogen decreases inside thefirst and second magnetostrictive films 3 a, 3 b, and hence internalstress hardly varies. Thus, the magnetostrictive characteristic isexpected to hardly vary.

In order to confirm this, output change rates were measured using theoutput change rate measurement samples 66 of FIG. 10 as shown in FIG.13. The output change rates measured were the change rate of thegradient (sensitivity) of the detected torque signal VS graph in FIG. 5,a so-called sensitivity change rate ΔVS, and the change rate of theoutput value (middle point) of the failure detection signal VE graph inFIG. 5, a so-called middle point change rate ΔVE.

In the measurement, first, the output change rate measurement samples 66were assembled in the electric power steering system 1 of FIG. 1, andthe initial sensitivity and middle point were measured. Thereafter, theoutput change rate measurement samples 66 were left at a use ambienttemperature of 110° C. for 400 hours. Then, the output change ratemeasurement samples 66 were assembled in the electric power steeringsystem 1 again, and the sensitivity and middle point after being left atthe use ambient temperature were measured. By dividing the differencethat is the sensitivity after being left at the use ambient temperatureminus the initial sensitivity by the initial sensitivity, thesensitivity change rate ΔVS was calculated. Likewise, by dividing thedifference that is the middle point after being left at the use ambienttemperature minus the initial middle point by the initial middle point,the middle point change rate ΔVE was calculated.

The output change rate measurement samples 66 and the TDS samples 65 onwhich three different types of heat treatments had been performed wereprepared. A first type is the one labeled “400° C. (HFH)” in FIG. 13 andhad been heat treated under the same conditions as with “400° C. (HFH)”in FIG. 12. A second type is the one labeled “400° C. (HFH)+annealing at180° C.” in FIG. 13 and had been heat treated under the same conditionsas with “400° C. (HFH)+2 hr annealing at 180° C.” in FIG. 12. A thirdtype is the one labeled “345° C. (HFH)” in FIG. 13 and had been heattreated under the same conditions as with “400° C. (HFH)” in FIG. 12except that heat treatment temperature is 345° C.

The horizontal axis of FIG. 13 represents the amount x of hydrogendesorbed by the time analysis temperature reached 400° C. when themeasurement according to the thermal desorption gas analysis wasperformed on the three types of TDS samples 65. The vertical axisrepresents the sensitivity and middle point change rates calculated fromthe measurements of the three types of output change rate measurementsamples 66. The use range of −5% to 5% of the output change rate can bethought to correspond to the use range Rvt of FIG. 5. If the outputchange rate is outside the use range of −5% to 5%, the failure detector19 determines that a failure has occurred, or the driver will feelunease when turning the steering wheel. Therefore, the heat treatmentprocess needs to be such that the output change rate is within the userange of −5% to 5%. Any of those three types of heat treatment processessatisfied that the output change rate is within the use range of −5% to5%. From the results of the three types of heat treatment processes, itwas found that there is a trend that as the amount x of hydrogendesorbed by the time analysis temperature reaches 400° C. increases, thesensitivity and middle point change rates also increase.

This trend shows that the more hydrogen is desorbed from the first andsecond magnetostrictive films 3 a, 3 b by the heat treatment process,the smaller amount x of hydrogen is desorbed at use ambient temperature,and hence the occurrence of the diffusive movement of hydrogen decreasesinside the first and second magnetostrictive films 3 a, 3 b, andinternal stress and thus the magnetostrictive characteristic hardlyvaries.

Thus, where the sensitivity change rate ΔVS is used as the output changerate, if the amount x of hydrogen desorbed by the time temperaturereaches 500° C. is at or below 15 ppm, it is satisfied that the outputchange rate is within the use range of −5% to 5%. Where the middle pointchange rate ΔVE is used as the output change rate, if the amount x ofhydrogen desorbed by the time temperature reaches 500° C. is at or below27 ppm, it is satisfied that the output change rate is within the userange of −5% to 5%.

In FIG. 14, the spectrum labeled “before heat treatment” and thespectrum labeled “400° C. (HFH)” of FIG. 12 are shown again. A spectrumestimated from these two spectra where the amount x of hydrogen desorbedby the time analysis temperature reaches 400° C. is at 15 ppm isindicated by an allowable amount 69. That is, as to the spectrum wherethe amount x of hydrogen desorbed by the time analysis temperaturereaches 400° C. is at 15 ppm, the amount x of hydrogen desorbed by thetime analysis temperature reaches 300° C. is expected to be 10 ppm, andthe amount x of hydrogen desorbed by the time analysis temperaturereaches 150° C. is expected to be 3 ppm.

Conversely, if the amount x of hydrogen desorbed by the time analysistemperature reaches 300° C. is at or below 10 ppm, it is expected to besatisfied that the sensitivity change rate is within the use range of−5% to 5%. Likewise, if the amount x of hydrogen desorbed by the timeanalysis temperature reaches 150° C. is at or below 3 ppm, it isexpected to be satisfied that the sensitivity change rate is within theuse range of −5% to 5. From the above, an allowable area 68 throughwhich spectra are allowed to pass can be set.

FIG. 15 shows a relationship between the heat treatment temperature andthe heat treatment time when the desorbed hydrogen amount x is the same.This desorbed hydrogen amount x is the amount that occurs in the casewhere the heat treatment temperature is at the use ambient temperatureof 110° C. and where the heat treatment time is 400 hours, which causesthe driver to realize that the auxiliary steering force differs inmagnitude between the rightward turning and leftward turning of thesteering wheel when performing stationary steering. The relationshipbetween the heat treatment temperature and the heat treatment time wasobtained by simulation from the activation energy and diffusioncoefficient of the diffusive movement of vacancies (like vacancy 57 inFIG. 9) in nickel of the same crystal structure, which is the maincomponent of the first and second magnetostrictive films 3 a, 3 b. Thus,it was found that the necessary heat treatment time is only 1.8 sec atthe heat treatment temperature of 400° C. This result is consistent withthe result shown in FIG. 13 where it is satisfied that the sensitivityand middle point change rates are within the use range of −5% to 5%,with the high frequency heating (HFH) of 400° C. in the heat treatmenttemperature and about 1 to 10 sec in the heat treatment time.

Further, from FIG. 15 it is expected to be satisfied that thesensitivity and middle point change rates are within the use range of−5% to 5% with the heat treatment temperature of 150° C. and the heattreatment time of 20 hours. Likewise, it is expected to be satisfiedthat the sensitivity and middle point change rates are within the userange of −5% to 5% with the heat treatment temperature of 300° C. andthe heat treatment time of 36 sec (10⁻² hr).

Therefore, the heat treatment temperature and the heat treatment time ofthe heat treatment process can be set according to the type ofheat-treating apparatus 61. For example, if a low-temperaturethermostatic bath whose heat treatment temperature cannot be set at ahigh temperature is used as the heat-treating apparatus 61, the heattreatment time may be set according to the low heat treatmenttemperature of the thermostatic bath. If a hardening or annealingapparatus whose heat treatment temperature is set at a high temperatureis used as the heat-treating apparatus 61, the heat treatment time maybe set according to the high heat treatment temperature. As such,degrees of freedom in selecting the heat-treating apparatus 61 can beincreased in number.

Moreover, the condition setting process of setting the heat treatmenttemperature and the heat treatment time based on the relationshipbetween the heat treatment temperature and the heat treatment time ofFIG. 15 may be performed before the heat treatment process. In thecondition setting process, the heat treatment time required to reducethe amount of hydrogen in the first and second magnetostrictive films 3a, 3 b can be set according to the heat treatment temperature.Conversely, the heat treatment temperature required to reduce the amountof hydrogen in the first and second magnetostrictive films 3 a, 3 b canbe set according to the heat treatment time.

As described above, as to vehicles, life worth of variation over timethat takes 400 hours can be accelerated with the heat treatment processof a short time, and thereafter the rate of variation over time can besuppressed. Therefore, there is provided a magnetostrictive torquesensor where even at the use ambient temperature the magnitude of thedetected steering torque signal does not shift and is the same betweenwhen turning the steering wheel rightward and when turning it leftwardwith the same steering effort.

What is claimed is:
 1. A production method for a magnetostrictive torquesensor which detects steering torque applied to a steering shaft byelectrically detecting distortion of a magnetostrictive film on asurface of the steering shaft, comprising: a plating step of forming themagnetostrictive film on the surface of the steering shaft; and a heattreatment step of heat treating the magnetostrictive film on the surfaceof the steering shaft; wherein the heat treatment step includes a heattreatment process for decreasing hydrogen included in themagnetostrictive film so that a hydrogen desorbing peak around 120° C.from the magnetostrictive film disappears when the magnetostrictive filmis heated after the heat treatment step.
 2. The production method forthe magnetostrictive torque sensor according to claim 1, wherein themagnetostrictive film is produced by the heat treatment step in whichthe magnetostrictive film is heated up to 400° C. for between 1 and 10seconds.
 3. The production method for the magnetostrictive torque sensoraccording to claim 1, wherein the heat treatment step includes a heattreatment process performed by high frequency heating and an annealingprocess performed for the steering shaft after the heat treatmentprocess.